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tanks; 5. an auxiliary assembly; 6. a solid propellant; 7. in respect to the size of the airframe; 8. to impart the propulsive thrust to the payload; 9. to assemble the airframe; 10. an integral part of the re-entry body; 11. to perform the guidance; 12. the use of an oxidizer; 13. whether liquid or solid

45. Прочтите и переведите без словаря:

1. We consider the re-entry body to be a main subsystem of the ballistic missile. 2. The re-entry body is to move towards the target. 3. The control signals are generated as a result of com­ mands from a guidance system. 4. An auxiliary power supply is

to give electric energy to various devices. 5. We know the mainstructure of the missile to be called the airframe. 6. The task of the student was to assemble and disassemble a pump. 7. You should know each stage of the two-stage liquid propellant vehicle to contain a rocket engine and two storage tanks. 8. The engineers consider a propulsive system to be a main part of the missile. 9. The combustion gases leave the engine through the exhaust nozzle. 10. The steering device is an integral part of any guided missile.

46. Найдите в тексте "Components of the Ballistic Missile" ответы на вопросы:

1. How is the airframe of the ballistic missile defined?

2.What does a turbopump assembly do?

3.What do the turbopump assemblies consist of? •4. How is the missile controlled in flight?

5. What signals

are generated as a result of commands from

a guidance system?

 

6.Do you know the re-entry body to contain the warhead, the fuze and the arming mechanism?

7.For what purpose has a rocket motor a thrust termination system?

8.What does a guidance system determine?

9.Is the solid-propellant vehicle simpler than its liquid-pro­ pellant counterpart?

47.Прочтите и переведите без словаря:

Some Characteristics of Guided Missile Components

All guided missiles must contain certain components in order to perform their functions. The missile must have a body

or basic structure; it must

be propelled; it must

be guided; and

it must carry

a payload.

The main

structure

of the

missile,

which contains

the other

components,

is called

the

airframe.

The component which moves the airframe is the propulsion system, or power plant. The component which makes the vehicle a real guided missile is the guidance system. If the missile is to

31

perform a military task, it must contain a payload consisting

of

a warhead and fuzes.

of the body

of

The airframe of a guided missile may consist

the weapon and the airfoils 1 which stabilize it

in flight and

control its path. We know the missile airframe to serve the same purpose as the airframe of an ordinary airplane: it carries the

necessary components and determines the

flight

characteristics

of the vehicle.

configuration — the shape and size

of the airfra­

The missile

m e— must be

the following:

1.

The body

and airfoils must

be

aerodynamically suitable for

the

speed at

which

the missile

is

to fly. 2. The airframe must be light in weight and sufficiently strong to withstand 12 great shock loads, vibrations, and accelera­ tions of high-speed flight. 3. The airframe must be easy to assem­ ble and to disassemble. The main components must form indepen-

'dent units. 4. The sections of the airframe must be simple in structure and easily fabricated. The sections are to be construe-, ted of material which is easy to work.

1airfoils — аэродинамические поверхности

2to withstand — выдерживать

48, Прочтите и переведите со словарем:

Propellant and Combustion Chamber

A considerable space in

the rocket is naturally occupied by

the propellant storage tanks

compartment. The more fuel the

rocket has, the farther it flies. The propellant stock of-the longrange modern missiles amounts to 80 per cent or more of their initial launching weight.

We know the propellant to consist of fuel and oxidizer. In normal conditions, in th$ furnace of a ship or locomotive for instance, the burning process is maintained by use of the oxygen in the air. This is practically non-existent at high altitudes. Therefore the rocket has to be provided with an oxidizer. Liquid oxygen or mixtures of “strong” nitric acid with special additives can be used for this purpose. Kerosene of various grades, alco­

hols and other substances are used as fuel. It should

be

noted

that the rocket carries much more

oxidizer

than

fuel.

This can

be seen from the following ratio:

14.8 kg

of air,

or

5.5

kg of

nitric acid, or 3.37 kg of liquid oxygen is required for complete combustion of 1 kg of kerosene.

The engineers consider the heart of the rocket to be its engine with the combustion chamber. This is a very powerful heating machine in which the fuel’s chemical energy is transformed into the kinetic energy of the gas jet. Its speed reaches 2.2-2.7 km/sec. As a .result a jet force is generated which easily carries a rocket to great distances.

Each second several hundred kilogrammes of fuel and oxidizer are injected into the combustion chamber through special injectors. This work is performed by a special assembly, called turbopump unit, located between the propellant storage tanks and the combustion chamber.

When the engine is in operation, the pressure inside the chamber may reach 50—60 atmospheres and the temperature 3,000—3,500° C. How can the materials withstand such a fantas­ tic temperature? The designers found a very clever solution for this. The. combustion chamber is double-walled, much like the cooling jacket of an automobile engine. Only instead of water,

one of the propellant components flows into

it. It

takes heat

from the chamber walls and thus is preheated

and

delivered to

the injectors.

 

 

Modern rockets are now equipped with solid-propellant engi­ nes as well. A solid mixture of fuel and oxidizer prepared in the form of blocks is filled into the rocket body, which in this case works as the combustion chamber.

2 П. И. Старостин

УРОК 4

Г р а м м а т и к а :

Сложное подлежащее (§ 7)

Т е к с т :

Rocket Engine

 

ПРЕДТЕКСТОВЫЕ

УПРАЖНЕНИЯ

 

 

 

49.

Прочтите

и переведите,

обращая

внимание

на

перевод

сложного

подлежащего:

 

 

 

 

 

 

 

 

 

 

 

 

1.

The nozzle

is

considered

to

be that

part

of

the

rocket

motor in which gases are accelerated to high velocities. 2. A

modern rocket

is known to be a complex mechanism consisting

of thousands of different parts. 3.

Satellites

launching

rocket

systems are known to have usually three or four stages. 4. The

payload is known to move along

a free-flight path

without

further expenditure of energy. 5. All the systems of the Salyut 4

were reported

to function

normally during

the

flight

of

the

station.

6. Jet

propulsion

systems

are

thought

to

be

reaction

motors because

they

operate on

the

reaction principle. 7. The

designers were

said

to

usethe

same

principle

of

retrieving

instrumentation. 8. The rocket is expected to drop smoothly to the Earth. 9. The steering device is thought to be an integral part of any guided missile. 10. The Moon is known to be the largest satellite of the solar system. 11. Single-stage rockets proved to be a means for launching payloads into a simple trajectory. 12. This satellite is certain to supply information on the earth radiation. 13. Three or more stages appeared to be necessary to achieve the required velocities to launch a minimum mass. 14. This propellant seemed to be suitable for a rocket engine. 15. This device turned out to be used in the latest designs of rockets. 16. The rocket engines are known to be divided into the main classes — the solid-propellant engines and the liquidpropellant engines. 17. Guided missiles are known to be divided into several classes depending on their launching method and type of the target, lfc. In modern long-range ballistic missiles

34

guidance is known to be achieved by a combination of gyrosco­ pes. 19. The design of a rocket propulsion is supposed to be influenced by many factors.

50. Прочтите слова и словосочетания:

to rely [ri'laij, relies upon this vehicle ['vi:ikl]; to eject [i:'d3ekt], ejection, by ejection of matter; original [э'пс^эп!), originally, originally carried within the vehicle; super, ['sjurpaj, supersonic ['sjuipa'somk], a supersonic stream, a supersonic

exhaust stream; either

['aiba], either solid or liquid; a combustion

[kom'bAst/anJ, a combustion chamber; to

oxidize

['oksidaiz],

an oxidizer, to burn in

an oxidizer; separate

['seprit],

a separate

chamber ['t/eimbo], a separate combustion chamber; molecules

j/molikju:lzJ, molecules of the gas; to

possess fpa'zes], to

possess large amounts of energy; uniform

['ju:mfo:m], uniformly,

uniformly directed

 

TEXT

 

ROCKET ENGINE

 

Propulsion for a ballistic vehicle usually relies upon a rocket system which is defined as propulsion by ejection of matter, all of which is originally carried within the vehicle which is being propelled. A rocket engine is known to produce an unbalanced force on the vehicle and is thus able to move it. The propulsive action of the rocket engine arises from the reaction to the acceleration, relative to the rocket engine, of a mass of propel­ lant originally carried within the rocket-propelled vehicle. In the rocket engines which are employed in ballistic missiles, accelera­ tion of the propellant mass is brought about by:

(a)releasing heat energy by a chemical reaction of propel­ lants within a combustion.chamber, and

(b)the use of an expansion nozzle to produce a supersonic

exhaust stream by expanding the evolved gas from combustionchamber pressure to ambient pressure.

The combustion chamber and expansion nozzle are together

known as the thrust chamber.

rocket

vehicles

can

be stored

Propellants which are used in

in either solid or liquid form, and

rocket

engines

are

considered

to be solidor liquid-propellant rocket engines respectively. The propellant tanks which are usually integral with the structure of the missile contain the propellants before their injection into the combustion chamber.

A rocket engine acts as a chamber containing a high-pressure gas which is continuously replenished as some of the gas escapes through an orifice into the region of lower pressure outside the

chamber. The

simplest rocket engine proves to

consist of

a

chamber — the

combustion chamber -^-.in which

fuel can

be

о*

 

 

35

 

 

 

burned in an oxidizer. The oxidizer can be carried either separately as in liquid propellants or mixed with the fuel as with solid propellants. The fuel and oxidizer are known as propel­ lants. In a liquid-propellant engine they are injected into the combustion chamber. In. a solid-propellant motor, the propellant storage tank and the combustion chamber are one and the same.

The

propellant

mixture is

triggered

electrically,

thermally,

or

chemically, to

produce a heat-releasing chemical

reaction,

and

the

molecules

of the gas

produced

by the combustion process

possess large amounts of energy, moving rapidly in all directions

within

the chamber. Individually these molecules have

a high

kinetic

energy .but

their motions

are randomly

directed.

To

achieve

a propulsive

effect, this

random motion

has

to

be

directed as uniformly as possible, in a direction away from the thrust chamber.

In exhausting through the expansion nozzle, the random motion of the gas particles is changed to a more directional motion. The gas emerges as a high-velocity stream from the thrust chamber.

The four components of a liquid-propellant engine are: 1 ) the feed system which is used to move jthe propellants from their storage tanks into the combustion chamber, 2 ) the thrust chamber where the propellants are burned and then expelled at

high

velocity, 3) a control system

which

starts, stops and

controls

the operation of the engine,

and 4)

auxiliary devices

such

as

means to deflect the jet to change the direction of the

thrust

vector.

 

 

Слова и словосочетания для запоминания

п

combustion

chamber, ejection, expansion nozzle,, feed

v

system, orifice, region, stream, thrust chamber

arise

(arose; arisen),

bring

about

(brought; brought),

 

emerge, escape, evolve, expel, inject, possess, propel,

a

release, replenish, store, trigger

 

 

ambient, random, supersonic

 

 

adv respectively,

uniformly

 

 

 

prep outside

 

 

 

 

 

 

 

УПРАЖНЕНИЯ

 

в

51.

Прочтите

и переведите, обращая внимание па перевод инфинитива

перфектной форме,

являющегося

часгыо

сложного

подлежащего:1

1 . This satellite was reported to have supplied information on the general structure of the ionosphere. 2 . In recent years the Soviet Union is known to have investigated the radio waves emitted by the Moon on frequencies within the range of 13—

35 cm. 3. Soviet scientists are considered to have done much for

36

the development of astronautics. 4. World meteorological centers are known to have been set up in Moscow and Washington and a direct communication channel has been established between them. 5. Two servo systems were considered to have been used during the powered flight to control position and velocity of this ballistic missile.. 6. The design of a rocket propulsion is believed to have been perfected.

52. Прочтите. Укажите номера предложений, содержащих инфинитив — часть сложного подлежащего. Переведите все предложения:

1. Propellants which are used in rocket vehicles are believed to be stored in either solid or liquid form. 2. The liquid rocket engine is known to consist of the combustion chamber, the feed system and the control system. 3. The turbojet engine is employ­ ed to propel certain guided missiles and aircraft in the high subsonic speed range. 4. We know the combustion chamber to be cooled by the oxidizer passing through a coolant space before

injecting into

the combustion chamber

through

a catalyzer.

5. The present

propulsion is considered

to employ

the energy

developed from combustion of fuel with the oxidizer. 6. A num­ ber of messages were known to be sent to the satellite where they were recorded and returned to the Earth at various points within the range of its radio-transmitters. 7. The observers are trained to recognize every object in the sky which they will see during the period of about 2 hours. 8. The orbits of the Soviet and American satellites are reported to be inclined approximately 25° to the polar plane. 9. Modern radar systems prove to be able to indicate the velocity of the aircraft with respect to the earth’s surface. 10. We were recommended to record the observations with the exact time of the passage of the satellite. 11. Some of the gas is certain to escape through an orifice into the region of lower pressure outside the chamber. 12. The thrust chamber is considered to be cooled by the passage of fuel through many, tubes making up its walls. 13. Rocket and missile development since 1930 is known to have resulted in launching instrumenta­ tion and manned vehicles into space. 14. They suppose most modern rocket motors to employ regenerative cooling in which the fuel must circulate around the combustion chamber and nozzle before it is injected for burning. 15. The speed of the reaction is found to be affected by the temperature of the propellant and the ambient temperature. 16. This satellite was designed to supply information on the general structure of the ionosphere. 17. The jet velocity of a rocket engine is considered to be the velocity at which the gases are ejected from the nozzle. 18. A missile is to be designed for the trajectory which it is expected to follow. 19. The powered flight of the ballistic missile appears to depend upon the energy that must be imparted to the payload.

37

53. Прочтите. Укажите номера предложений, в которых выделенное сло­ во является сказуемым. Переведите все предложения:

1 .

The

analysis of these

data

means that

all

the

systems

function normally. 2. These devices are the auxiliary means for

feeding the propellant into the combustion chamber. 3.

The

development of entirely new compatible means of spaceships

docking

is the

problem of

greatest importance. 4.

This means

that if a man exerts a force of 150 pounds on the car, the car

exerts an equal and opposite force of

150 pounds

bn

the

man.

5. An important means of man’s penetration into near space is

the setting-up

and flight

of

orbital

scientific

stations

with

rotating crews. 6. A ballistic missile flies the greater part of its trajectory as a freely thrown body; this means that it is acted upon only by two forces: the earth’s gravitation and the resistance

of the

air. 7. Propellants rich in hydrogen and other light

elements are advantageous because they lead to a low mean

molecular weight of the exhaust gas.

 

54.

Прочтите и переведите,

обращая ' внимание

на перевод союза

“either...

or”:

 

 

1 .

Propellants which

are used in rocket

vehicles are known

to be stored in either solid or liquid form. 2. Launching of a missile is carried out either from-open ground emplacements or from underground silos. 3. The release of heat away from the vehicle can* be accomplished'either by the action of strong shock waves or by radiation .of heat away from the hot surface of the vehicle. 4. Short-range missiles may be used against either fixed or moving targets. 5. Such satellite can contain either television cameras or photographic equipment for transmitting pictures to the Earth. 6. The oxidizer can be carried either separately as in liquid propellants or mixed with the fuel as with solid propel­

lants.

7.

The spaceship

is

controlled

either

automatically or

manually by the cosmonaut.

 

 

 

 

 

 

 

 

55.

Определите

по

суффиксам,

к каким частям

речи

относятся

слова,

и переведите их:

 

 

 

 

 

 

 

 

 

 

 

1 .

 

oxidizer; 2. oxidation; 3. injection; 4. injector; 5. superso­

nic; 6.

respective;

7.

respectively;

8.

uniformly; 9.

ejection;*

1 0. storage;

1 1 . expansion; 1 2 . propulsive

 

 

 

 

 

56.

Прочтите и

переведите,. обращая-' внимание на

значение

отрицатель­

ного префикса "un-”:1

 

 

 

 

 

 

 

 

 

 

1 . balanced,

unbalanced;

2 .

distributed,,

undistributed;

3. desirable, undesirable; 4. reliable, unreliable; 5. accomplished,

unaccomplished; 6. achievable, unachievable; 7. attached,

unat­

tached;

 

8.

available,

unavailable;

9.

changed,

unchanged;

1 0. restricted, unrestricted;

1 1 . usable,

unusable;

1 2 . successful,

unsuccessful

 

 

 

 

 

 

 

 

 

 

 

 

38

57. К каждому словосочетанию подберите русский эквивалент:

1 . to bring about the accele­

1 . воспламенять

 

топливную

 

ration of

the

.propellant

 

смесь

 

 

 

 

 

 

mass

 

 

 

 

2. выбрасываться

через

соп­

2 . to use a feed system

 

3. to

replenish the

storage

3.

ловое отверстие

 

 

камера

ракетного двига­

4.

tanks

the

 

'

4.

теля

 

 

 

тепловую

outside

combustion

высвобождать

 

5.

chamber

 

 

 

 

5.

энергию

 

 

 

сверхзвуко­

ejection of matter

 

производить

 

 

 

 

 

 

 

 

 

вую струю

выхлопных га­

6. to propel a rocket

 

 

зов

 

 

распределен­

 

6. равномерно

7. to

produce

a

supersonic

7.

ный окислитель

 

 

сверхзвуковое сопло

 

 

exhaust

stream

 

 

8. вызывать

ускорение

мас­

8. a thrust chamber

 

9. to escape through an ori­

 

сы топлива

в движение

ра­

9. приводить

 

fice

 

 

 

 

 

кету

 

 

 

вещества

10. a random motion

 

10. выбрасывание

 

1 1 . to

release heat

energy

И. вне камеры сгорания

 

1 2 . an expansion nozzle

 

12. пополнять топливные баки

13.

a

uniformly

distributed

13.

беспорядочное движение

14.

oxidizer

 

the

propellant

14.

использовать

систему

по­

to

trigger

 

mixture

 

 

 

 

 

дачи (топлива)

 

 

 

58.

Прочтите и переведите без словаря:

 

 

 

 

 

 

 

1 .

to'

expel

the

gas from a

combustion chamber; 2. the

propellant

mixture

triggered

electrically;

3.

the

randomly

directed motions; 4. to possess high kinetic energy; 5 an ambient pressure; 6. to arise from the reaction to the acceleration; 7. to employ an expansion nozzle; 8. the respectively changing thrust; 9. to bring about a supersonic stream; 10. to expel gases at high velocity; 1 1 . a region of lower pressure; 12. the gas emerged as a high velocity stream from the thrust chamber

59. ГТрочтите и переведите без словаря:

1. The propellant mixture is triggered and produces a heatreleasing chemical reaction. 2. The random motion of molecules

has to be directed as uniformly as possible. 3. An expansion ^nozzle is known to be. used to produce a supersonic exhaust stream. 4. The propellants must be stored in either solid or liquid form. 6. The storage tanks are replenished from time to time; 6. The gas is expected to escape through an orifice into the

39

region of lower pressure. 7. In a liquid-propellant engine the propellants are injected into the combustion, chamber. 8. These molecules seem to possess great amount of energy.

60. Найдите в тексте "Rocket Engine" ответы на вопросы:

1. What is'acceleration of the propellant mass in the rocket engines brought about by?

2. In what form can propellants in rocket vehicles be stored?

3.How can the oxidizer be carried?

4.What motion is the random motion of the gas particles changed to in exhausting through the expansion nozzle?

5. How many basic components of a liquid rocket engine are there?

6.How is the propellant mixture triggered?

7.What reaction does the propulsive action of the rocket engine arise from?

8.Are the combustion chamber and expansion nozzle together known as the thrust chamber?

61.К каждому слову подберите русский эквивалент:

1.

solid

1. обладать

2. to bring about

2.

агрегат

3. to

propel

3.

окислитель

4.

region

4.

в отношении

5.

to

desire

5.

выделять

6.

to

store

6.

сообщать

7.

airframe

7.

появляться

8. to emerge

8.

возникать

9. control

9.

выбрасываться

10. respectively

10.

приводить в движение

11. to impart

И. окружающий

12.

to evolve

12.

неотъемлемый

13.

assembly

13.

корпус {ракеты)

14.

to escape

14.

желать

15.

to

arise

15.

управление

16.

oxidizer

16.

вызывать

17.

ambient

17.

хранить

18.

in respect (to)

18.

твердый

19.

to

possess

19.

соответственно

20.

integral

20.

область

62. Прочтите и переведите без словаря:

General Characteristics of the Turbojet Engine

This engine is known to consist of a diffuser *, a mechanical compressor, a combustion chamber, a mechanical turbine, and an exhaust nozzle. The function of the diffuser is to transform

40